EP1931567B8 - Mat d'accrochage de turboreacteur pour aeronef - Google Patents

Mat d'accrochage de turboreacteur pour aeronef Download PDF

Info

Publication number
EP1931567B8
EP1931567B8 EP06793901.7A EP06793901A EP1931567B8 EP 1931567 B8 EP1931567 B8 EP 1931567B8 EP 06793901 A EP06793901 A EP 06793901A EP 1931567 B8 EP1931567 B8 EP 1931567B8
Authority
EP
European Patent Office
Prior art keywords
lateral
aircraft
mounting structure
turbine engine
engine mounting
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP06793901.7A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP1931567A1 (fr
EP1931567B1 (fr
Inventor
Lionel Diochon
Jean-Michel Cetout
Laurent Lafont
David Chartier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of EP1931567A1 publication Critical patent/EP1931567A1/fr
Application granted granted Critical
Publication of EP1931567B1 publication Critical patent/EP1931567B1/fr
Publication of EP1931567B8 publication Critical patent/EP1931567B8/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Body Structure For Vehicles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Assembled Shelves (AREA)
  • Connection Of Plates (AREA)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)
EP06793901.7A 2005-10-03 2006-09-29 Mat d'accrochage de turboreacteur pour aeronef Not-in-force EP1931567B8 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0552989A FR2891526B1 (fr) 2005-10-03 2005-10-03 Mat d'accrochage de turboreacteur pour aeronef
PCT/EP2006/066873 WO2007039556A1 (fr) 2005-10-03 2006-09-29 Mat d'accrochage de turboreacteur pour aeronef

Publications (3)

Publication Number Publication Date
EP1931567A1 EP1931567A1 (fr) 2008-06-18
EP1931567B1 EP1931567B1 (fr) 2012-04-04
EP1931567B8 true EP1931567B8 (fr) 2018-08-08

Family

ID=36577371

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06793901.7A Not-in-force EP1931567B8 (fr) 2005-10-03 2006-09-29 Mat d'accrochage de turboreacteur pour aeronef

Country Status (10)

Country Link
US (1) US8070093B2 (ru)
EP (1) EP1931567B8 (ru)
JP (1) JP4864975B2 (ru)
CN (1) CN100548803C8 (ru)
AT (1) ATE552173T1 (ru)
BR (1) BRPI0616578B1 (ru)
CA (1) CA2624457C (ru)
FR (1) FR2891526B1 (ru)
RU (1) RU2399558C9 (ru)
WO (1) WO2007039556A1 (ru)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AR057484A1 (es) 2005-08-04 2007-12-05 Bayer Healthcare Llc Dispositvo de puncion pequeno
FR2920198B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Structure pour inverseur de poussee
FR2920409B1 (fr) 2007-08-27 2009-12-18 Airbus France Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
FR2928136B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
FR2928181B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central.
FR2928347B1 (fr) * 2008-03-07 2010-06-25 Aircelle Sa Structure d'accrochage pour turboreacteur
US20140174056A1 (en) * 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
FR2936493A1 (fr) * 2008-10-01 2010-04-02 Aircelle Sa Mat adapte pour supporter un turboracteur d'aeronef et nacelle associee a un mat.
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2965548B1 (fr) * 2010-10-01 2012-10-19 Airbus Operations Sas Mat d'accrochage d'un moteur d'aeronef comprenant deux attaches voilure avant a pions de cisaillement orthogonaux
FR2981046B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
CN102849218A (zh) * 2012-09-04 2013-01-02 西安飞机工业（集团）有限责任公司 一种飞机辅助动力装置安装梁
WO2015010315A1 (en) 2013-07-26 2015-01-29 Mra Systems, Inc. Aircraft engine pylon
FR3012793B1 (fr) * 2013-11-05 2017-05-05 Airbus Operations Sas Ensemble pour aeronef comprenant une ferrure fixee sur la partie extrados d'un caisson de voilure, pour le montage d'un mat d'accrochage sur ce caisson de voilure
CN103569367B (zh) * 2013-11-13 2015-08-26 中国航空工业集团公司西安飞机设计研究所 机翼吊装涡扇发动机飞机的发动机挂架
BR112016010876B1 (pt) 2013-11-18 2022-02-01 Lord Corporation Sistema de fixação de motor e método de fixação de um motor turboélice
FR3015434B1 (fr) * 2013-12-23 2017-12-08 Snecma Suspension de turbomachine
FR3040076B1 (fr) * 2015-08-13 2017-08-11 Airbus Operations Sas Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau
FR3065442B1 (fr) * 2017-04-25 2021-03-19 Airbus Operations Sas Ensemble moteur pour aeronef comprenant une attache moteur avant integree au caisson du mat d'accrochage
JP2019131071A (ja) * 2018-01-31 2019-08-08 三菱重工業株式会社 航空機
US10806087B2 (en) * 2018-05-21 2020-10-20 Deere & Company Fan support arm
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
FR3129376A1 (fr) * 2021-11-19 2023-05-26 Airbus Operations Mat réacteur pour coupler un turboréacteur à une aile d’un aéronef

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US4206893A (en) * 1978-09-27 1980-06-10 The Boeing Company Seal closure for slot in engine mounting strut
SU849694A1 (ru) * 1980-03-12 1996-09-20 А.А. Бобух Устройство для крепления двухконтурного турбореактивного двигателя
RU2104228C1 (ru) * 1993-07-01 1998-02-10 Самарское государственное научно-производственное предприятие "Труд" Устройство для крепления авиационного двигателя к самолету
US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
FR2793768B1 (fr) * 1999-05-17 2001-09-07 Aerospatiale Airbus Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif
FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
US7104306B2 (en) * 2004-06-14 2006-09-12 The Boeing Company Cast unitized primary truss structure and method

Also Published As

Publication number Publication date
CA2624457C (en) 2013-09-24
FR2891526A1 (fr) 2007-04-06
BRPI0616578A2 (pt) 2012-12-25
US20080315033A1 (en) 2008-12-25
WO2007039556A1 (fr) 2007-04-12
FR2891526B1 (fr) 2007-11-02
EP1931567A1 (fr) 2008-06-18
US8070093B2 (en) 2011-12-06
CN100548803C (zh) 2009-10-14
BRPI0616578B1 (pt) 2018-10-23
CN101272952A (zh) 2008-09-24
JP2009509847A (ja) 2009-03-12
RU2399558C9 (ru) 2019-12-30
EP1931567B1 (fr) 2012-04-04
WO2007039556A8 (fr) 2009-06-11
ATE552173T1 (de) 2012-04-15
RU2399558C2 (ru) 2010-09-20
RU2008117402A (ru) 2009-11-10
CA2624457A1 (en) 2007-04-12
JP4864975B2 (ja) 2012-02-01
CN100548803C8 (zh) 2018-06-29
BRPI0616578A8 (pt) 2018-05-08

Similar Documents

Publication Publication Date Title
EP1931567B8 (fr) Mat d'accrochage de turboreacteur pour aeronef
DE602005003719D1 (de) Flugzeugcockpitboden
BR112015020833A2 (pt) veículo de duas rodas, e, método para montar um veículo de duas rodas
DE602006005387D1 (de) Triebwerkanordnung für flugzeug
CN100548803B8 (zh) 航空器的涡轮喷气发动机支架
FR2915178B1 (fr) Attache d'un caisson de mat sur une voilure, pincant un panneau lateral du caisson
MX2009003267A (es) Rejilla moldeada por inyeccion para bastidores de tamiz de sacudidor.
ATE452823T1 (de) Strukturgondel
DE602006016180D1 (de) Flugzeugrumpfmontagekonzept
RU2008125086A (ru) Отсек шасси с раздельной конструкцией
WO2010031958A3 (fr) Partie arriere d'aeronef comprenant deux demi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef
ATE330844T1 (de) Aufhängung eines triebwerks unter einer flugzeugflügel
ATE420817T1 (de) Triebwerkmontagestruktur für ein flugzeug
FR2878229B1 (fr) Systeme de fixation d'un mat de moteur a l'aile d'un aeronef
MY141638A (en) Tail fairing designed with features for suppression of vortices addition between fairings, apparatus incorporating such fairings, methods of making and using such fairings and apparatus, and methods of installing such fairings
WO2004066351A3 (en) Mounting for solar panels
ATE428632T1 (de) Flugzeugmotoranordnung
WO2008096087A3 (fr) Section de fuselage pour aeronef et aeronef comprenant une telle section
WO2008093003A8 (fr) Nacelle pour turboréacteur double flux
ATE418492T1 (de) Turbojet für flugzeug, mit solch einem turbojet ausgestattetes flugzeug und verfahren zur befestigung solch eines turbojets an einem flugzeug
WO2009032027A3 (en) Harness with mounted engine frame
MY142820A (en) A shroud mounting structure of a motorcycle
AU2003224226A1 (en) Engine pylon suspension attachment of an engine under an aircraft wing section
WO2009135975A3 (es) Dispositivo para retirar e instalar componentes de aeronave
WO2009012917A3 (en) Improvements in or relating to seating

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20080313

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: AIRBUS OPERATIONS

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

RTI1 Title (correction)

Free format text: TURBINE ENGINE MOUNTING STRUCTURE FOR AIRCRAFT

DAX Request for extension of the european patent (deleted)
GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 552173

Country of ref document: AT

Kind code of ref document: T

Effective date: 20120415

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602006028643

Country of ref document: DE

Effective date: 20120531

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20120404

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 552173

Country of ref document: AT

Kind code of ref document: T

Effective date: 20120404

LTIE Lt: invalidation of european patent or patent extension

Effective date: 20120404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120804

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120806

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120705

BERE Be: lapsed

Owner name: AIRBUS OPERATIONS

Effective date: 20120630

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120630

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

26N No opposition filed

Effective date: 20130107

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602006028643

Country of ref document: DE

Effective date: 20130101

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120630

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120715

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120630

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130101

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120629

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120630

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120704

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120629

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20060629

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

GRAT Correction requested after decision to grant or after decision to maintain patent in amended form

Free format text: ORIGINAL CODE: EPIDOSNCDEC

PLAA Information modified related to event that no opposition was filed

Free format text: ORIGINAL CODE: 0009299DELT

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 13

REG Reference to a national code

Ref country code: CH

Ref legal event code: PK

Free format text: DAS ANMELDEDATUM WURDE AUF 29.09.2006 BERICHTIGT

R26N No opposition filed (corrected)

Effective date: 20130107

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20210920

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20220922

Year of fee payment: 17

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20220929

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220929

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230930